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Paint System, Fluorescent, Removable, for Aircraft Application
- Aerospace Material Specification
- AMSP21600B
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification establishes the requirements for a high visibility, durable, exterior fluorescent coating system consisting of a pigmented fluorescent coating with a clear protective overcoat containing a weathering stabilizer. This coating system is capable of being removed without softening the permanent undercoats.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
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Topic
Data Sets - Support Documents
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| TABLE 1 | COMPOSITION | |
| TABLE 2 | PROPERTIES | |
| TABLE 3 | COLOR LIMITS BEFORE AND AFTER WEATHERING FOR RED-ORANGE | |
| TABLE 4 | COLOR LIMITS BEFORE AND AFTER WEATHERING FOR YELLOW-ORANGE | |
| TABLE 5 | FORMULA FOR REMOVER | |
| TABLE 6 | TOLERANCE | |
| TABLE 7 | TEST METHODS | |
| TABLE 8 | WHITE TEST PAINT FORMULA | |
| TABLE 9 | FLUORESCENT COATING | |
| TABLE 10 | CLEAR OVERCOAT |
Issuing Committee
AMS G8 Aerospace Organic Coatings Committee
The AMS Committee G-8, Aerospace Organic Coatings, provides a forum to address common concerns such as application, corrosion, environmental compliance, material compatibility, OSHA requirements, performance requirements, specifications, surface preparation, and test methods. The three primary areas of activity are: 1. Writing and Maintaining Specifications 2. Cooperative Testing 3. Information Sharing and Networking
Reference
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